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Y 3.N 21/5:6/1784
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Flight investigation in climb and at high speed or a two-blade and three-blade propeller / |
1 |
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Y 3.N 21/5:6/1785
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Friction coefficients in the inlet length of smooth round tubes / |
1 |
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Y 3.N 21/5:6/1786
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Recommendations for numerical solution of reinforced panel and fuselage-ring problems / |
1 |
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Y 3.N 21/5:6/1787
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Comparison of the structural efficiency of panels having straight-web and curved web Y-section stiffeners / |
1 |
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Y 3.N 21/5:6/1788
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Flight tests of an apparatus for varying dihedral effect in flight / |
1 |
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Y 3.N 21/5:6/1789
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Investigation of aerodynamic and icing conditions of recessed fuel-vent configurations / |
1 |
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Y 3.N 21/5:6/1790
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Investigation of icing characteristics of typical light-airplane engine induction systems / |
1 |
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Y 3.N 21/5:6/1791
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Corrosion tests of a heated wing utilizing an exhaust-gas-air mixture for ice prevention / |
1 |
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Y 3.N 21/5:6/1792
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Study by the Prandtl-Glauert method of compressibility effects and critical Mach number for ellipsoids of various aspect ratios and thickness ratios / |
1 |
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Y 3.N 21/5:6/1793
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Investigation of meteorological conditions associated with aircraft icing in layer-type clouds for 1947-48 winter / |
1 |
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Y 3.N 21/5:6/1794
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Gust-tunnel investigation of a wing model with semichord line swept back 30 degrees / |
1 |
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Y 3.N 21/5:6/1795
|
Application of radial-equilibrium condition to axial-flow compressor and turbine design / |
1 |
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Y 3.N 21/5:6/1796
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Theoretical analysis of oscillations of a towed cable / |
1 |
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Y 3.N 21/5:6/1797
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A Study of stall phenomena on a 45 degree swept-forward wing / |
1 |
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Y 3.N 21/5:6/1798
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Effect of thickness on the lateral force and yawing moment of a sideslipping delta wing at supersonic speeds / |
1 |
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Y 3.N 21/5:6/1799
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On the flying qualities of helicopters / |
1 |
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Y 3.N 21/5:6/1800
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Laminar mixing of a compressible fluid / |
1 |
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Y 3.N 21/5:6/1801
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Wind-tunnel investigation of the spinning characteristics of a model of a twin-tail low-wing personal-owner-type airplane with linked and unlinked rudder and aileron controls / |
1 |
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Y 3.N 21/5:6/1802
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Wind-tunnel investigation of an NACA 65-210 semispan wing equipped with circular plug ailerons and a full-span slotted flap / |
1 |
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Y 3.N 21/5:6/1803
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Downwash in the vertical and horizontal planes of symmetry behind a triangular wing in supersonic flow / |
1 |
